CN117600536B - Carrier rocket cabin section inner wall processing device - Google Patents
Carrier rocket cabin section inner wall processing device Download PDFInfo
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- CN117600536B CN117600536B CN202310300273.7A CN202310300273A CN117600536B CN 117600536 B CN117600536 B CN 117600536B CN 202310300273 A CN202310300273 A CN 202310300273A CN 117600536 B CN117600536 B CN 117600536B
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- 238000012545 processing Methods 0.000 title claims abstract description 85
- 238000003801 milling Methods 0.000 claims description 10
- 238000003754 machining Methods 0.000 claims description 8
- 238000009434 installation Methods 0.000 claims description 7
- 238000012546 transfer Methods 0.000 claims description 5
- 238000013461 design Methods 0.000 abstract description 12
- 238000000034 method Methods 0.000 abstract description 5
- 239000000463 material Substances 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 4
- 230000003287 optical effect Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 230000002708 enhancing effect Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 230000001965 increasing effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C3/00—Milling particular work; Special milling operations; Machines therefor
- B23C3/02—Milling surfaces of revolution
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q1/00—Members which are comprised in the general build-up of a form of machine, particularly relatively large fixed members
- B23Q1/25—Movable or adjustable work or tool supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q5/00—Driving or feeding mechanisms; Control arrangements therefor
- B23Q5/22—Feeding members carrying tools or work
- B23Q5/34—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission
- B23Q5/38—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission feeding continuously
- B23Q5/40—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission feeding continuously by feed shaft, e.g. lead screw
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- Mechanical Engineering (AREA)
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Abstract
The application provides a carrier rocket cabin inner wall processing device, which comprises a bottom plate, wherein a supporting device is rotatably arranged on the bottom plate along a first axis direction, a first driving device is connected to the supporting device, and the first driving device is used for driving the supporting device to move around the first axis direction; the support device is sleeved with a processing assembly, the processing assembly is connected with a second driving device, the second driving device is used for driving the processing assembly to move along the first axis direction, the support device is sleeved with a positioning assembly, the positioning assembly is positioned between the bottom plate and the processing assembly, and the positioning assembly is fixedly connected with the bottom plate; through the structure, the processing assembly finishes processing the inner wall of the cabin section according to the design scheme, so that the aim of reducing the weight of the cabin section of the carrier rocket is fulfilled, and the quality of the cabin section meets the design requirement; in the processing process, the processing is completed without changing different equipment, so that the processing cost and the processing period are reduced, and meanwhile, the manpower and the material resources are saved.
Description
Technical Field
The present disclosure relates generally to the field of carrier rocket processing technology, and in particular, to a device for processing an inner wall of a carrier rocket cabin.
Background
The carrier rocket is an important mark of the construction aerospace country of China, and is also a strategic tool for maintaining the space safety of China and pushing the space exploration of China to expand to more remote deep space. The development of carrier rocket designs key components such as rocket body structure system, power system, control system, ground launching system and the like, and is a complex system engineering. In the whole arrow body structure, the cabin section plays roles of connecting the storage tanks and mounting the carrier for the instrument and equipment, and is an important bearing section with huge size and complex structure; because the outer surface of the cabin section is provided with the pneumatic appearance, in order to enable the quality of the cabin section of the carrier rocket to meet the design requirement, the inner wall of the cabin section is required to be processed so as to achieve the purpose of reducing the weight of the cabin section.
In the prior art, a large numerical control machine tool is generally adopted to machine the inner wall of the cabin according to a design scheme, so that the machining cost is increased, and meanwhile, different working procedures are completed by different equipment during machining, so that a machining cycle process is caused, and a large amount of manpower and material resources are occupied.
Disclosure of Invention
In view of the foregoing drawbacks and deficiencies of the prior art, it is desirable to provide a device for processing an inner wall of a rocket bay for a vehicle that addresses the foregoing problems.
The application provides a processing device for the inner wall of a cabin section of a carrier rocket, which comprises the following components:
A bottom plate;
the supporting device is rotatably arranged on the bottom plate along the first axis direction, and is connected with a first driving device which is used for driving the supporting device to rotate around the first axis direction;
The processing assembly is sleeved on the supporting device and is used for processing the cabin section of the carrier rocket; the processing assembly is connected with a second driving device, and the second driving device is used for driving the processing assembly to move along the first axis direction; the first axis direction is perpendicular to the bottom plate;
the positioning assembly is sleeved on the supporting device and positioned between the bottom plate and the processing assembly, and the positioning assembly is fixedly connected with the bottom plate.
According to the technical scheme provided by the embodiment of the application, the supporting device comprises a supporting rod arranged along the first axis direction, and a first mounting seat and a second mounting seat which are respectively arranged at two ends of the supporting rod along the first axis direction, wherein a mounting cavity is arranged in the supporting rod, and two ends of the mounting cavity along the first axis direction are provided with switching shafts; one end, far away from the supporting rod, of the second mounting seat is fixedly connected with the bottom plate; the support rod is connected with the first mounting seat through a first bearing, the support rod is connected with the second mounting seat through a second bearing, the second mounting seat is hollow, the first driving device is arranged in the second mounting seat, the driving end of the first driving device is connected with the switching shaft, and the first driving device is used for driving the switching shaft to drive the support rod to rotate around the first axis direction.
According to the technical scheme provided by the embodiment of the application, the transfer shaft is provided with the third through hole along the first axis direction, the second driving device is arranged in the mounting cavity along the first axis direction, the two ends of the second driving device along the first axis direction are arranged in the third through hole, and the second driving device is connected with the transfer shaft through a third bearing; the support rod is provided with a first channel communicated with the mounting cavity along the first axis direction, the processing assembly is sleeved on the support rod, and the processing assembly penetrates through the first channel to be connected with the second driving device; the second direction is perpendicular to the first axis direction.
According to the technical solution provided by the embodiment of the present application, the second driving device includes:
the lead screw is arranged in the mounting cavity along the first axis direction, and the lead screw is connected with the switching shaft through the third bearing; the screw rod is in threaded connection with the processing assembly;
the second driving motor is installed in the second installation seat and fixedly connected with the switching shaft, the driving end of the second driving motor is connected with the screw rod, and the second driving motor is used for driving the screw rod to rotate around the first axis direction.
According to the technical scheme provided by the embodiment of the application, the processing assembly comprises:
The connecting seat is sleeved on the screw rod, the connecting seat is in threaded connection with the screw rod, one end, far away from the screw rod, of the connecting seat penetrates through the first channel to be connected with a fixing ring, the fixing ring is sleeved on the supporting rod, and the fixing ring is connected with an electric cylinder;
The third driving motor is connected with the driving end of the electric cylinder, and the electric cylinder is used for changing the rotary motion of the motor into linear motion; the driving end of the third driving motor is connected with a milling cutter, and the milling cutter is used for machining the inner wall of the cabin section.
According to the technical scheme provided by the embodiment of the application, the connecting seat comprises: the nut is sleeved on the screw rod, the nut is in threaded connection with the screw rod, the adapter plate is arranged at one end, away from the screw rod, of the nut, and the other end of the adapter plate penetrates through the first channel and is fixedly connected with the fixing ring.
According to the technical scheme provided by the embodiment of the application, the adapter plate penetrates through the first channel to be connected with the sliding sleeve, the electric cylinder is fixedly installed in the sliding sleeve, the sliding sleeve is connected with the motor adapter seat, the motor adapter seat is provided with the first through hole along the second direction, the third driving motor is arranged in the first through hole, and the third driving motor is connected with the driving end of the electric cylinder.
According to the technical scheme provided by the embodiment of the application, the positioning assembly comprises: the first wallboard is sleeved on the supporting rod and is positioned between the second mounting seat and the processing assembly; the second wall plate and the third wall plate are respectively arranged at two sides of the supporting rod along the second direction, and are respectively and fixedly connected with the bottom plate; the first wall plate is fixedly connected with the second wall plate and the third wall plate.
According to the technical scheme provided by the embodiment of the application, the top of the first mounting seat is provided with the fourth wallboard.
According to the technical scheme provided by the embodiment of the application, the shaft sleeve is arranged between the adapter shaft and the third bearing.
The application has the beneficial effects that:
based on the technical scheme provided by the application, the processing device for the inner wall of the carrier rocket cabin section comprises a bottom plate, wherein a supporting device is rotatably arranged on the bottom plate along the first axis direction, and is connected with a first driving device which is used for driving the supporting device to move around the first axis direction; the support device is sleeved with a processing assembly, the processing assembly is connected with a second driving device, the second driving device is used for driving the processing assembly to move along the first axis direction, the support device is sleeved with a positioning assembly, the positioning assembly is positioned between the bottom plate and the processing assembly, and the positioning assembly is fixedly connected with the bottom plate; when the carrier rocket positioning device is used, a cabin section of a carrier rocket to be processed is placed around the supporting device, the cabin section is fixed on the positioning assembly, the first driving device is started to control the supporting device to rotate around the first axis direction according to a design scheme, the processing assembly sleeved on the supporting device is driven to rotate, and meanwhile the second driving device is started to drive the processing assembly to move along the first axis direction; the processing assembly is used for finishing the processing of the inner wall of the cabin section according to a design scheme so as to achieve the purpose of reducing the weight of the cabin section of the carrier rocket, and further the quality of the cabin section meets the design requirement; in the processing process, the processing is completed without changing different equipment, so that the processing cost and the processing period are reduced, and meanwhile, the manpower and the material resources are saved.
Drawings
Other features, objects and advantages of the present application will become more apparent upon reading of the detailed description of non-limiting embodiments, made with reference to the accompanying drawings in which:
FIG. 1 is a schematic view of a device for processing the inner wall of a carrier rocket bay according to the present application;
FIG. 2 is a schematic view of a support apparatus and a processing assembly of the present application;
FIG. 3 is a cross-sectional view of a support device and tooling assembly of the present application;
FIG. 4 is an enlarged partial view of portion A of FIG. 3;
Fig. 5 is a partial enlarged view of a portion B shown in fig. 3.
In the figure: 1. a bottom plate; 2. a first wall plate; 3. a second wall plate; 4. a cabin section; 5. a support rod; 6. a fourth wall plate; 7. a third bearing; 8. a third wall plate; 9. a shaft sleeve; 10. a transfer shaft; 11. a second bearing; 12. a first mount; 14. a screw rod; 15. a nut; 16. an adapter plate; 17. a third driving motor; 18. an electric cylinder; 19. a motor adapter; 20. a sliding sleeve; 21. a first bearing; 22. a fixing ring; 23. a first driving device; 24. a second mounting base; 25. and a second driving motor.
Detailed Description
The application is described in further detail below with reference to the drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the application and are not limiting of the application. It should be noted that, for convenience of description, only the portions related to the application are shown in the drawings.
It should be noted that, without conflict, the embodiments of the present application and features of the embodiments may be combined with each other. The application will be described in detail below with reference to the drawings in connection with embodiments.
Referring to fig. 1-2, a schematic diagram of a device for processing an inner wall of a cabin of a carrier rocket according to the present application includes:
A base plate 1;
the support device is rotatably arranged on the bottom plate 1 along the first axis direction, a first driving device 23 is connected to the support device, and the first driving device 23 is used for driving the support device to rotate around the first axis direction;
The processing assembly is sleeved on the supporting device and is used for processing the cabin section 4 of the carrier rocket; the processing assembly is connected with a second driving device, and the second driving device is used for driving the processing assembly to move along the first axis direction; the first axis direction is perpendicular to the bottom plate 1;
The positioning assembly is sleeved on the supporting device and is positioned between the bottom plate 1 and the processing assembly, and the positioning assembly is fixedly connected with the bottom plate 1.
In some embodiments, the first driving device 23 is a servo motor and a transmission, wherein the transmission is connected to the driving end of the servo motor, and the driving end of the transmission is connected to the supporting device; controlling the rotation speed of the supporting device through the speed changer, thereby controlling the rotation speed of the processing assembly;
Specifically, the first axis direction is a vertical direction;
Specifically, in this embodiment, the cabin segment 4 is placed on the positioning assembly by glue;
Working principle: when the carrier rocket positioning device is used, the cabin section 4 of the carrier rocket to be processed is placed around the supporting device, the cabin section 4 is fixed on the positioning component, the first driving device 23 is started to control the supporting device to rotate around the first axis direction according to the design scheme, the processing component sleeved on the supporting device is driven to rotate, and meanwhile the second driving device is started to drive the processing component to move up and down along the vertical direction; the processing assembly is enabled to finish processing the inner wall of the cabin section 4 according to a design scheme, so that the purpose of weight reduction of the cabin section 4 of the carrier rocket is achieved, and the quality of the cabin section 4 meets the design requirement; in the processing process, the processing is completed without changing different equipment, so that the processing cost and the processing period are reduced, and meanwhile, the manpower and the material resources are saved.
In some embodiments, the supporting device comprises a supporting rod 5 arranged along the first axis direction, and a first mounting seat 12 and a second mounting seat 24 respectively arranged at two ends of the supporting rod 5 along the first axis direction, wherein a mounting cavity is arranged in the supporting rod 5, and two ends of the mounting cavity along the first axis direction are provided with a switching shaft 10; one end of the second mounting seat 24, which is far away from the supporting rod 5, is fixedly connected with the bottom plate 1; the support rod 5 is connected with the first mounting seat 12 through a first bearing 21, the support rod 5 is connected with the second mounting seat 24 through a second bearing 11, the second mounting seat 24 is hollow, the first driving device 23 is arranged in the second mounting seat 24, the driving end of the first driving device 23 is connected with the switching shaft 10, and the first driving device 23 is used for driving the switching shaft 10 to drive the support rod 5 to rotate around the first axis direction.
Specifically, as shown in fig. 3, the supporting device includes a supporting rod 5 disposed along the first axis direction, and a first mounting seat 12 and a second mounting seat 24 respectively disposed at two ends of the supporting rod 5 along the first axis direction, a mounting cavity is disposed inside the supporting rod 5, and two ends of the mounting cavity along the first axis direction are provided with a switching shaft 10; one end of the second mounting seat 24, which is far away from the supporting rod 5, is fixedly connected with the bottom plate 1; in this embodiment, the support rod 5 is an optical axis, as shown in fig. 4 and 5, the optical axis is connected with the first mounting seat 12 through a first bearing 21, the optical axis is connected with the second mounting seat 24 through a second bearing 11, and in this embodiment, the first bearing 21 and the second bearing 11 are both crossed roller bearings; the second mounting seat 24 is hollow, the first driving device 23 is arranged in the second mounting seat 24, and the driving end of the first driving device 23 is connected with the adapter shaft 10; the first driving device 23 is a servo motor and a transmission, the first driving device 23 drives the adapter shaft 10 to rotate around the first axis direction, and further drives the optical axis to rotate around the first axis direction, and when the optical axis rotates, the first mounting seat 12 and the second mounting seat 24 keep motionless under the action of the crossed roller bearing.
In some embodiments, a third through hole is formed in the adapter shaft 10 along the first axis direction, the second driving device is disposed in the mounting cavity along the first axis direction, two ends of the second driving device along the first axis direction are disposed in the third through hole, and the second driving device is connected with the adapter shaft 10 through a third bearing 7; the support rod 5 is provided with a first channel communicated with the mounting cavity along the first axis direction, the processing component is sleeved on the support rod 5, and the processing component passes through the first channel and is connected with the second driving device; the second direction is perpendicular to the first axis direction.
Specifically, in this embodiment, the third bearing 7 is a ball bearing;
Specifically, the second direction is a horizontal direction;
Specifically, as shown in fig. 4 and 5, the second driving device is disposed in the mounting cavity along the first axis direction, and the second driving device is connected with the adapting shaft 10 through the third bearing 7, and when the second driving device drives the processing assembly to move along the first axis direction, under the action of the third bearing 7, the adapting shaft 10 is kept motionless, so that the supporting rod 5 is kept motionless.
In certain embodiments, the second driving means comprises:
the lead screw 14 is arranged in the mounting cavity along the first axis direction, and the lead screw 14 is connected with the adapter shaft 10 through the third bearing 7; the lead screw 14 is in threaded connection with the processing assembly;
The second driving motor 25, the second driving motor 25 is installed in the second installation seat 24 and fixedly connected with the adapter shaft 10, the driving end of the second driving motor 25 is connected with the screw rod 14, and the second driving motor 25 is used for driving the screw rod 14 to rotate around the first axis direction.
Specifically, the second driving device includes a lead screw 14 and a second driving motor 25, and in this embodiment, the second driving motor 25 is a servo motor; because the screw 14 is in threaded connection with the processing assembly, when the second driving motor 25 drives the screw 14 to rotate around the first axis direction, the processing assembly moves on the screw 14 along the first axis direction; simultaneously, under the action of the third bearing 7, the supporting rod 5 does not rotate along with the screw rod 14; so that the displacement position and the displacement direction of any of the machining modules are adjusted according to the design when machining the cabin segment 4.
In certain embodiments, the processing assembly comprises:
The connecting seat is sleeved on the screw rod 14, the connecting seat is in threaded connection with the screw rod 14, one end, far away from the screw rod 14, of the connecting seat penetrates through the first channel to be connected with a fixed ring 22, the fixed ring 22 is sleeved on the supporting rod 5, and the fixed ring 22 is connected with an electric cylinder 18;
A third driving motor 17, the third driving motor 17 is connected with the driving end of the electric cylinder 18, and the electric cylinder 18 is used for changing the rotation motion of the motor into linear motion; the driving end of the third driving motor 17 is connected with a milling cutter, and the milling cutter is used for machining the inner wall of the cabin section 4.
Specifically, the electric cylinder 18 is a modularized product integrating a servo motor and a screw rod, and converts the rotary motion of the servo motor into linear motion; the electric cylinder 18 is used for driving the third driving motor 17 to move towards the inner wall direction of the cabin section 4;
in some embodiments, the third drive motor 17 is a spindle motor;
Specifically, since the screw rod 14 is in threaded connection with the connection seat, when the second driving motor 25 drives the screw rod 14 to rotate around the first axis direction, the connection seat moves on the screw rod 14 along the first axis direction; further, the milling cutter is driven to move along the first axis direction, and meanwhile, the electric cylinder 18 drives the milling cutter to move towards the inner wall direction of the cabin section 4; when the milling cutter contacts with the inner wall of the cabin section 4, the third driving motor 17 drives the milling cutter to rotate, so that the inner wall of the cabin section 4 is processed.
In certain embodiments, the connector comprises: the nut 15 is sleeved on the screw rod 14, the nut 15 is in threaded connection with the screw rod 14, the adapter plate 16 is arranged at one end, far away from the screw rod 14, of the nut 15, and the other end of the adapter plate 16 penetrates through the first channel and is fixedly connected with the fixing ring 22.
Specifically, the nut 15 is sleeved on the screw rod 14, the nut 15 is in threaded connection with the screw rod 14, and when the screw rod 14 rotates, the nut 15 moves along the screw rod 14; an adapter plate 16 is disposed at an end of the nut 15 away from the screw 14, and the adapter plate 16 is used for connecting the nut 15 with a fixing ring 22.
In some embodiments, the adapter plate 16 is connected with a sliding sleeve 20 through the first channel, the electric cylinder 18 is fixedly mounted in the sliding sleeve 20, a motor adapter 19 is connected to the sliding sleeve 20, a first through hole is formed in the motor adapter 19 along the second direction, the third driving motor 17 is disposed in the first through hole, and the third driving motor 17 is connected with the driving end of the electric cylinder 18.
Specifically, the adapter plate 16 is connected with a sliding sleeve 20 through the first channel, the electric cylinder 18 is fixedly installed in the sliding sleeve 20, and the sliding sleeve 20 is used for enhancing the installation stability of the electric cylinder 18;
Specifically, the sliding sleeve 20 is connected with a motor adapter 19, the motor adapter 19 is provided with a first through hole along the second direction, the third driving motor 17 is disposed in the first through hole, and the driving end of the electric cylinder 18 is connected with the third driving motor 17; the motor adapter 19 is used for enhancing the stability of the installation of the third driving motor 17.
In certain embodiments, the positioning assembly comprises: the first wall plate 2, the second wall plate 3 and the third wall plate 8 are sleeved on the supporting rod 5, and are positioned between the second mounting seat 24 and the processing assembly; the second wall plate 3 and the third wall plate 8 are respectively arranged at two sides of the supporting rod 5 along the second direction, and the second wall plate 3 and the third wall plate 8 are respectively fixedly connected with the bottom plate 1; the first wall plate 2 is fixedly connected with the second wall plate 3 and the third wall plate 8.
Specifically, the second wall plate 3 and the third wall plate 8 are respectively disposed at two sides of the support rod 5 along the horizontal direction, the second wall plate 3 and the third wall plate 8 are disposed along the vertical direction, and bottoms of the second wall plate 3 and the third wall plate 8 are fixedly connected with the bottom plate 1 through screws; the first wall plate 2 is sleeved on the supporting rod 5 and is positioned between the second mounting seat 24 and the processing assembly, and two ends of the first wall plate 2 along the second direction are fixedly connected with the second wall plate 3 and the third wall plate 8 through screws respectively;
When the cabin section 4 of the carrier rocket is processed, the cabin section 4 to be processed is placed around the supporting rods 5, and the cabin section 4 is fixed on the first wall plate 2 through glue; the positioning component is used for positioning the cabin section 4 and enhancing the stability of the support rod 5 during processing.
In some embodiments, the top of the first mount 12 is provided with a fourth wall plate 6.
Specifically, the top of the first mounting seat 12 is provided with a fourth wall plate 6, and the fourth wall plate 6 is used for enhancing the stability of the support rod 5 when the cabin segment 4 is processed.
In some embodiments, a sleeve 9 is provided between the adapter shaft 10 and the third bearing 7.
Specifically, a shaft sleeve 9 is disposed between the adapter shaft 10 and the electric bearing, and the shaft sleeve 9 is used for fixing the position of the third bearing 7 and increasing the service life of the third bearing 7.
The above description is only illustrative of the preferred embodiments of the present application and of the principles of the technology employed. It will be appreciated by persons skilled in the art that the scope of the application referred to in the present application is not limited to the specific combinations of the technical features described above, but also covers other technical features formed by any combination of the technical features described above or their equivalents without departing from the inventive concept. Such as the above-mentioned features and the technical features disclosed in the present application (but not limited to) having similar functions are replaced with each other.
Claims (9)
1. A carrier rocket cabin section inner wall processingequipment, characterized by comprising:
A bottom plate (1);
the support device is rotatably arranged on the bottom plate (1) along a first axis direction, a first driving device (23) is connected to the support device, and the first driving device (23) is used for driving the support device to rotate around the first axis direction;
The supporting device comprises a supporting rod (5) arranged along the first axis direction, and a first mounting seat (12) and a second mounting seat (24) which are respectively arranged at two ends of the supporting rod (5) along the first axis direction, wherein an installation cavity is arranged in the supporting rod (5), and two ends of the installation cavity along the first axis direction are provided with switching shafts (10); one end, far away from the supporting rod (5), of the second mounting seat (24) is fixedly connected with the bottom plate (1); the support rod (5) is connected with the first mounting seat (12) through a first bearing (21), the support rod (5) is connected with the second mounting seat (24) through a second bearing (11), the second mounting seat (24) is hollow, the first driving device (23) is arranged in the second mounting seat (24), the driving end of the first driving device (23) is connected with the switching shaft (10), and the first driving device (23) is used for driving the switching shaft (10) to drive the support rod (5) to rotate around the first axis direction;
The processing assembly is sleeved on the supporting device and is used for processing a cabin section (4) of the carrier rocket; the processing assembly is connected with a second driving device, and the second driving device is used for driving the processing assembly to move along the first axis direction; the first axis direction is perpendicular to the bottom plate (1);
the positioning assembly is sleeved on the supporting device and is positioned between the bottom plate (1) and the processing assembly, and the positioning assembly is fixedly connected with the bottom plate (1).
2. A carrier rocket cabin inner wall processing device according to claim 1, wherein a third through hole is formed in the transfer shaft (10) along the first axis direction, the second driving device is arranged in the mounting cavity along the first axis direction, two ends of the second driving device along the first axis direction are arranged in the third through hole, and the second driving device is connected with the transfer shaft (10) through a third bearing (7); the support rod (5) is provided with a first channel communicated with the mounting cavity along the first axis direction, the processing assembly is sleeved on the support rod (5), and the processing assembly penetrates through the first channel and is connected with the second driving device.
3. A launch vehicle bay inner wall processing device according to claim 2, wherein the second drive means comprises:
The lead screw (14) is arranged in the mounting cavity along the first axis direction, and the lead screw (14) is connected with the adapter shaft (10) through the third bearing (7); the lead screw (14) is in threaded connection with the processing assembly;
The second driving motor (25), the second driving motor (25) is installed in the second installation seat (24) and fixedly connected with the switching shaft (10), the driving end of the second driving motor (25) is connected with the screw rod (14), and the second driving motor (25) is used for driving the screw rod (14) to rotate around the first axis direction.
4. A launch vehicle bay inner wall processing device according to claim 3, wherein the processing assembly comprises:
The connecting seat is sleeved on the screw rod (14), the connecting seat is in threaded connection with the screw rod (14), one end, far away from the screw rod (14), of the connecting seat penetrates through the first channel to be connected with a fixed ring (22), the fixed ring (22) is sleeved on the supporting rod (5), and the fixed ring (22) is connected with an electric cylinder (18);
A third driving motor (17), wherein the third driving motor (17) is connected with the driving end of the electric cylinder (18), and the electric cylinder (18) is used for changing the rotation motion of the motor into linear motion; the driving end of the third driving motor (17) is connected with a milling cutter, and the milling cutter is used for machining the inner wall of the cabin section (4).
5. A launch vehicle bay inner wall processing device as defined in claim 4, wherein the connector comprises: the nut (15) is sleeved on the screw rod (14), the nut (15) is in threaded connection with the screw rod (14), the adapter plate (16) is arranged at one end, far away from the screw rod (14), of the nut (15), and the other end of the adapter plate (16) penetrates through the first channel and is fixedly connected with the fixing ring (22).
6. A device for processing the inner wall of a cabin section of a carrier rocket according to claim 4, wherein a sliding sleeve (20) is connected to the fixing ring (22), the electric cylinder (18) is fixedly installed in the sliding sleeve (20), a motor adapter (19) is connected to the sliding sleeve (20), a first through hole is formed in the motor adapter (19) along a second direction, the third driving motor (17) is arranged in the first through hole, and the third driving motor (17) is connected with the driving end of the electric cylinder (18); the second direction is perpendicular to the first axis direction.
7. A launch vehicle bay inner wall processing device as defined in claim 6, wherein the positioning assembly comprises: the first wallboard (2), the second wallboard (3) and the third wallboard (8), wherein the first wallboard (2) is sleeved on the supporting rod (5) and is positioned between the second mounting seat (24) and the processing assembly; the second wall plate (3) and the third wall plate (8) are respectively arranged at two sides of the supporting rod (5) along the second direction, and the second wall plate (3) and the third wall plate (8) are respectively fixedly connected with the bottom plate (1); the first wall plate (2) is fixedly connected with the second wall plate (3) and the third wall plate (8).
8. A device for processing the inner wall of a rocket section according to claim 7, wherein the top of the first mounting base (12) is provided with a fourth wall plate (6).
9. A device for processing the inner wall of a rocket cabin according to claim 2, wherein a shaft sleeve (9) is arranged between the adapter shaft (10) and the third bearing (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310300273.7A CN117600536B (en) | 2023-03-27 | 2023-03-27 | Carrier rocket cabin section inner wall processing device |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1345189A (en) * | 1971-04-06 | 1974-01-30 | Le Progres Charbonnier En Abre | Milling machines |
| JPH1094911A (en) * | 1996-09-25 | 1998-04-14 | Kawasaki Heavy Ind Ltd | Work method of semispherical shell internal wall surface |
| CN108515215A (en) * | 2017-12-04 | 2018-09-11 | 北京航天新风机械设备有限责任公司 | A kind of nacelle inner wall robot milling automatic processing unit (plant) |
| CN112405006A (en) * | 2020-12-04 | 2021-02-26 | 福州大学 | Integral automatic drilling and riveting device for cylindrical shell and working method of integral automatic drilling and riveting device |
| CN214108893U (en) * | 2020-12-31 | 2021-09-03 | 常州朱美拉模具技术有限公司 | Vertical machining equipment for forming annular die oblique angle |
| CN115365554A (en) * | 2022-10-25 | 2022-11-22 | 溧阳市江南烘缸制造有限公司 | Quick forming machine tool for Yankee dryer groove |
-
2023
- 2023-03-27 CN CN202310300273.7A patent/CN117600536B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1345189A (en) * | 1971-04-06 | 1974-01-30 | Le Progres Charbonnier En Abre | Milling machines |
| JPH1094911A (en) * | 1996-09-25 | 1998-04-14 | Kawasaki Heavy Ind Ltd | Work method of semispherical shell internal wall surface |
| CN108515215A (en) * | 2017-12-04 | 2018-09-11 | 北京航天新风机械设备有限责任公司 | A kind of nacelle inner wall robot milling automatic processing unit (plant) |
| CN112405006A (en) * | 2020-12-04 | 2021-02-26 | 福州大学 | Integral automatic drilling and riveting device for cylindrical shell and working method of integral automatic drilling and riveting device |
| CN214108893U (en) * | 2020-12-31 | 2021-09-03 | 常州朱美拉模具技术有限公司 | Vertical machining equipment for forming annular die oblique angle |
| CN115365554A (en) * | 2022-10-25 | 2022-11-22 | 溧阳市江南烘缸制造有限公司 | Quick forming machine tool for Yankee dryer groove |
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